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CAS IR Grid
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力学研究所 [1]
长春光学精密机械与物... [1]
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OAI收割 [2]
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会议论文 [2]
发表日期
2012 [1]
2011 [1]
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Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300
会议论文
OAI收割
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
作者:
Qi DW
;
He GW(何国威)
;
Liu YM
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浏览/下载:60/0
  |  
提交时间:2013/02/26
Aerospace engineering
Deformation
Exhibitions
Flexible wings
Reynolds number
Rigidity
Vortex flow
Aerodynamic forces
Chord-based Reynolds number
Flexural rigidities
Free stream
Free-stream flow
Lattice boltzmann
Leading-edge vortices
Lift coefficient
Lift force
Particle methods
Pitch rate
Power efficiency
Reduced frequency
Three dimensional space
Time-periods
Tip edge
Trailing edges
Trailing vortex
LOS rate reconstruction and application of roll-pitch seeker (EI CONFERENCE)
会议论文
OAI收割
2nd Annual Conference on Electrical and Control Engineering, ICECE 2011, September 16, 2011 - September 18, 2011, Yichang, China
Yang C.
;
Zhang N.
;
Jia H.
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浏览/下载:22/0
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提交时间:2013/03/25
Frame motion form of roll-pitch seeker is introduced in this paper. There is corresponding relationship between the frame angle of the roll-pitch seeker and the traditional yaw-pitch seeker. The discrepancy of line-of-sight (LOS) rate of the two seekers is caused by the different frame motion forms. LOS rate reconstruction method of roll-pitch seeker is deduced. Compared to the pure proportional navigation guidance law
the true proportional navigation guidance law is more suitable for the roll-pitch seeker missile guidance. 2011 IEEE.